Honeywell International Inc. KSN770 用户手册
Draft
Page 1-4
6 Dec 2012
34-70-06
SYSTEM INSTALLATION MANUAL
066-01204 / 066-01213
© Honeywell International Inc. Do not copy without express permission of Honeywell.
1.5
Units Supplied
1.5.1
KSN 7xx Safety Navigator
Refer to Table 1-1 for the available configurations.
1.5.2
GPS Antennas
The KA 96 GPS active antenna, PN 071-01620-0001 is the designated antenna for the KSN 770 Safety
Navigator, and must be ordered separately.
Navigator, and must be ordered separately.
1.6
License Requirements
An aircraft radio station license is no longer required for the KSN 7xx models that transmit for domestic
(US) operations. For international travel, forms can be obtained from your nearest FCC field office or
found online at http://transition.fcc.gov/Forms/Form605/605.html/ (See the regulatory authority for all
countries in which the KSN 7xx will be operated for more information).
(US) operations. For international travel, forms can be obtained from your nearest FCC field office or
found online at http://transition.fcc.gov/Forms/Form605/605.html/ (See the regulatory authority for all
countries in which the KSN 7xx will be operated for more information).
1.7
Recommendations for IFR Approval
The following functions are required for IFR certification of the KSN 7xx.
A.
Aircraft Logbook Entry
B.
Aircraft Installation Requirements
(1)
TSO’d Antenna
The antenna must be a TSO’d KA 96 GPS antenna, PN 071-01620-0001 or equivalent.
(2)
NAV Instrumentation
The navigation information (D-Bar, NAV Flag, and TO-FROM) must be displayed on an
instrument in the pilot’s panel within the pilot’s field of view. Electromechanical indicators are
capable of displaying the variable scale factors of enroute, terminal, and approach modes. If
the NAV information is displayed on an EFIS system, it must be capable of displaying variable
D-Bar scaling required for GPS approaches. This may require a modification to the EFIS
system. Refer to SECTION III - SYSTEM INTERCONNECT for the typical indicator usage.
instrument in the pilot’s panel within the pilot’s field of view. Electromechanical indicators are
capable of displaying the variable scale factors of enroute, terminal, and approach modes. If
the NAV information is displayed on an EFIS system, it must be capable of displaying variable
D-Bar scaling required for GPS approaches. This may require a modification to the EFIS
system. Refer to SECTION III - SYSTEM INTERCONNECT for the typical indicator usage.
(3)
OBS Interface
For approach approval, the OBS resolver must be interfaced so that selected course through
the HSI/CDI indicator will be sent to the KSN 7xx for D-Bar resolution. In mechanical
indicators, it will be accomplished by switching the OBS resolver lines; in EFIS installations,
it will usually be through the serial busses. Some EFIS applications may require an adapter.
Refer to SECTION III - SYSTEM INTERCONNECT for further information regarding OBS
resolver characteristics.
the HSI/CDI indicator will be sent to the KSN 7xx for D-Bar resolution. In mechanical
indicators, it will be accomplished by switching the OBS resolver lines; in EFIS installations,
it will usually be through the serial busses. Some EFIS applications may require an adapter.
Refer to SECTION III - SYSTEM INTERCONNECT for further information regarding OBS
resolver characteristics.
Hardware
RTCA/DO-254 Levels B and C
Table 1-3. KSN 770 Safety Navigator Leading Particulars (Cont)
Characteristic
Specification
Draft as of 10/15/2012